|
Selected(0)Clear
Items/Page: Sort: |
| Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades 期刊论文
VIRTUAL AND PHYSICAL PROTOTYPING, 2023, 卷号: 18, 期号: 1, 页码: e2235680
Authors: Qu DD(屈丹丹) ; Lin X(林鑫); Zhang K(张坤); Li ZY(李志永); Wang ZZ(王泽众); Liu GL(刘国亮); Meng Y(孟洋); Luo GX(罗耕星); Wang RY(王若岩); Yu XL(余西龙)
 Adobe PDF(4980Kb) |  Favorite | View/Download：176/4 | Submit date：2023/09/05
Hybrid rocket engine additive manufacturing three-dimensional printing breathable blade composite fuel grain mechanical and combustion properties porous structure > |
| 特征结构对复合式石蜡基药柱燃烧特性的影响研究 期刊论文
推进技术, 2023, 页码: 9
Authors: 张泽林; 林鑫; 王若岩; 罗家枭; 王泽众; 张春元; 李飞; 余西龙
Adobe PDF(1532Kb) | Favorite | View/Download：144/44 | Submit date：2023/05/08
固液混合火箭发动机 复合式药柱 特征结构 尺度 燃烧特性 |
| 基于光学诊断的某新型含铝推进剂燃烧特性分析 期刊论文
爆炸与冲击, 2023, 页码: 12
Authors: 杨云杰; 邢时越; 张少华; 余西龙; 王泽众; 王海燕
Adobe PDF(1310Kb) | Favorite | View/Download：89/31 | Submit date：2023/05/08
固体推进剂 铝 激光点火 燃烧特性 光学诊断 |
| Charactering Catalytic Ignition and Combustion for the Ninety Percent Hydrogen Peroxide/Paraffin Based Hybrid Rocket Engine 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023
Authors: Wang ZZ(王泽众); Lin X(林鑫); Wu K(吴坤); Zhang ZL(张泽林); Fang SH(方思晗); Meng DD(孟东东); Li F(李飞); Yu XL(余西龙)
Adobe PDF(712Kb) | Favorite | View/Download：84/8 | Submit date：2023/04/20
Hybrid Rocket Engines Propellant Thermocouples Numerical Analysis Catalysis Absorption Spectroscopy Combustion Products decomposition efficiency Paraffin Fuel Ignition Systems |
| Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023
Authors: Luo JX(罗家枭); Zhang ZL(张泽林); Lin X(林鑫); Wang ZZ(王泽众); Wu K(吴坤); Zhou GX(周功喜); Zhang SH(张森豪); Li F(李飞); Yu XL(余西龙); Wu, Jie
Adobe PDF(732Kb) | Favorite | View/Download：55/2 | Submit date：2023/04/20
Combustion Instability Rayleigh Scattering Precombustion Chamber Hybrid Propellant Rocket Hybrid Rocket Motor Mass Flow Rate Convective Heat Transfer Characteristic Velocity Planar Laser Induced Fluorescence Propulsion and Power |
